JP5546732B2 - インピンジメント冷却式バケットシュラウド、該シュラウドが組み込まれたタービンロータ並びに冷却方法 - Google Patents
インピンジメント冷却式バケットシュラウド、該シュラウドが組み込まれたタービンロータ並びに冷却方法 Download PDFInfo
- Publication number
- JP5546732B2 JP5546732B2 JP2008003924A JP2008003924A JP5546732B2 JP 5546732 B2 JP5546732 B2 JP 5546732B2 JP 2008003924 A JP2008003924 A JP 2008003924A JP 2008003924 A JP2008003924 A JP 2008003924A JP 5546732 B2 JP5546732 B2 JP 5546732B2
- Authority
- JP
- Japan
- Prior art keywords
- cooling
- shroud
- airfoil
- impingement
- turbine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000001816 cooling Methods 0.000 title claims description 90
- 239000012809 cooling fluid Substances 0.000 claims description 17
- 238000004891 communication Methods 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 8
- 239000012530 fluid Substances 0.000 claims description 6
- 238000007599 discharging Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 description 14
- 238000013461 design Methods 0.000 description 6
- 238000012546 transfer Methods 0.000 description 5
- 239000002184 metal Substances 0.000 description 2
- 238000005266 casting Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008685 targeting Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/33—Shrouds which are part of or which are rotating with the rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/652,483 | 2007-01-12 | ||
US11/652,483 US7568882B2 (en) | 2007-01-12 | 2007-01-12 | Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2008169845A JP2008169845A (ja) | 2008-07-24 |
JP5546732B2 true JP5546732B2 (ja) | 2014-07-09 |
Family
ID=39510081
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008003924A Active JP5546732B2 (ja) | 2007-01-12 | 2008-01-11 | インピンジメント冷却式バケットシュラウド、該シュラウドが組み込まれたタービンロータ並びに冷却方法 |
Country Status (5)
Country | Link |
---|---|
US (1) | US7568882B2 (zh) |
JP (1) | JP5546732B2 (zh) |
CN (1) | CN101235728B (zh) |
CH (1) | CH703144B1 (zh) |
DE (1) | DE102008003412B4 (zh) |
Families Citing this family (60)
Publication number | Priority date | Publication date | Assignee | Title |
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GB0724612D0 (en) * | 2007-12-19 | 2008-01-30 | Rolls Royce Plc | Rotor blades |
US8348612B2 (en) * | 2008-01-10 | 2013-01-08 | General Electric Company | Turbine blade tip shroud |
US8322986B2 (en) * | 2008-07-29 | 2012-12-04 | General Electric Company | Rotor blade and method of fabricating the same |
US8408868B2 (en) * | 2008-12-30 | 2013-04-02 | General Electric Company | Methods, systems and/or apparatus relating to inducers for turbine engines |
GB0901129D0 (en) * | 2009-01-26 | 2009-03-11 | Rolls Royce Plc | Rotor blade |
CH700319A1 (de) | 2009-01-30 | 2010-07-30 | Alstom Technology Ltd | Gekühltes bauelement für eine gasturbine. |
US8096767B1 (en) * | 2009-02-04 | 2012-01-17 | Florida Turbine Technologies, Inc. | Turbine blade with serpentine cooling circuit formed within the tip shroud |
US8096772B2 (en) * | 2009-03-20 | 2012-01-17 | Siemens Energy, Inc. | Turbine vane for a gas turbine engine having serpentine cooling channels within the inner endwall |
CH700686A1 (de) * | 2009-03-30 | 2010-09-30 | Alstom Technology Ltd | Schaufel für eine gasturbine. |
CH700687A1 (de) * | 2009-03-30 | 2010-09-30 | Alstom Technology Ltd | Gekühltes bauteil für eine gasturbine. |
US8337158B1 (en) * | 2009-10-22 | 2012-12-25 | Florida Turbine Technologies, Inc. | Turbine blade with tip cap |
EP2436884A1 (en) | 2010-09-29 | 2012-04-04 | Siemens Aktiengesellschaft | Turbine arrangement and gas turbine engine |
US8684664B2 (en) * | 2010-09-30 | 2014-04-01 | General Electric Company | Apparatus and methods for cooling platform regions of turbine rotor blades |
US8777568B2 (en) * | 2010-09-30 | 2014-07-15 | General Electric Company | Apparatus and methods for cooling platform regions of turbine rotor blades |
US8840369B2 (en) * | 2010-09-30 | 2014-09-23 | General Electric Company | Apparatus and methods for cooling platform regions of turbine rotor blades |
US8851845B2 (en) * | 2010-11-17 | 2014-10-07 | General Electric Company | Turbomachine vane and method of cooling a turbomachine vane |
CN102128055A (zh) * | 2011-04-21 | 2011-07-20 | 西北工业大学 | 一种带冠的燃气涡轮冷却叶片 |
US9127560B2 (en) * | 2011-12-01 | 2015-09-08 | General Electric Company | Cooled turbine blade and method for cooling a turbine blade |
US10138736B2 (en) | 2012-01-20 | 2018-11-27 | General Electric Company | Turbomachine blade tip shroud |
US9109455B2 (en) * | 2012-01-20 | 2015-08-18 | General Electric Company | Turbomachine blade tip shroud |
US9249667B2 (en) * | 2012-03-15 | 2016-02-02 | General Electric Company | Turbomachine blade with improved stiffness to weight ratio |
US9322282B2 (en) | 2012-11-30 | 2016-04-26 | General Electric Company | Fillet for use with a turbine rotor blade tip shroud |
US9759070B2 (en) | 2013-08-28 | 2017-09-12 | General Electric Company | Turbine bucket tip shroud |
US9664118B2 (en) | 2013-10-24 | 2017-05-30 | General Electric Company | Method and system for controlling compressor forward leakage |
US9435212B2 (en) * | 2013-11-08 | 2016-09-06 | Siemens Energy, Inc. | Turbine airfoil with laterally extending snubber having internal cooling system |
US10494929B2 (en) | 2014-07-24 | 2019-12-03 | United Technologies Corporation | Cooled airfoil structure |
US9835087B2 (en) * | 2014-09-03 | 2017-12-05 | General Electric Company | Turbine bucket |
US10774654B2 (en) * | 2015-07-31 | 2020-09-15 | General Electric Company | Cooling arrangements in turbine blades |
US10006294B2 (en) | 2015-10-19 | 2018-06-26 | General Electric Company | Article and method of cooling an article |
US10508554B2 (en) | 2015-10-27 | 2019-12-17 | General Electric Company | Turbine bucket having outlet path in shroud |
US9885243B2 (en) * | 2015-10-27 | 2018-02-06 | General Electric Company | Turbine bucket having outlet path in shroud |
US10156145B2 (en) * | 2015-10-27 | 2018-12-18 | General Electric Company | Turbine bucket having cooling passageway |
US10202852B2 (en) | 2015-11-16 | 2019-02-12 | General Electric Company | Rotor blade with tip shroud cooling passages and method of making same |
US10184342B2 (en) | 2016-04-14 | 2019-01-22 | General Electric Company | System for cooling seal rails of tip shroud of turbine blade |
US10344599B2 (en) * | 2016-05-24 | 2019-07-09 | General Electric Company | Cooling passage for gas turbine rotor blade |
US10364685B2 (en) | 2016-08-12 | 2019-07-30 | Gneral Electric Company | Impingement system for an airfoil |
US10436048B2 (en) | 2016-08-12 | 2019-10-08 | General Electric Comapny | Systems for removing heat from turbine components |
US10443397B2 (en) | 2016-08-12 | 2019-10-15 | General Electric Company | Impingement system for an airfoil |
US10408062B2 (en) | 2016-08-12 | 2019-09-10 | General Electric Company | Impingement system for an airfoil |
CN106451865A (zh) * | 2016-11-21 | 2017-02-22 | 南京磁谷科技有限公司 | 一种高速电机冷却结构 |
US20180216474A1 (en) * | 2017-02-01 | 2018-08-02 | General Electric Company | Turbomachine Blade Cooling Cavity |
US10746029B2 (en) | 2017-02-07 | 2020-08-18 | General Electric Company | Turbomachine rotor blade tip shroud cavity |
US10472974B2 (en) | 2017-02-14 | 2019-11-12 | General Electric Company | Turbomachine rotor blade |
US10533747B2 (en) * | 2017-03-30 | 2020-01-14 | General Electric Company | Additively manufactured mechanical fastener with cooling fluid passageways |
US11242767B2 (en) * | 2017-05-01 | 2022-02-08 | General Electric Company | Additively manufactured component including an impingement structure |
US11060407B2 (en) * | 2017-06-22 | 2021-07-13 | General Electric Company | Turbomachine rotor blade |
US20190003320A1 (en) * | 2017-06-30 | 2019-01-03 | General Electric Company | Turbomachine rotor blade |
US10301943B2 (en) * | 2017-06-30 | 2019-05-28 | General Electric Company | Turbomachine rotor blade |
US10590777B2 (en) * | 2017-06-30 | 2020-03-17 | General Electric Company | Turbomachine rotor blade |
FR3070424B1 (fr) * | 2017-08-29 | 2020-07-03 | Safran Aircraft Engines | Roue de turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion |
US11156102B2 (en) * | 2018-03-19 | 2021-10-26 | General Electric Company | Blade having a tip cooling cavity and method of making same |
KR102141998B1 (ko) * | 2018-09-05 | 2020-08-06 | 두산중공업 주식회사 | 블레이드슈라우드, 터빈 및 이를 포함하는 가스터빈 |
US11339668B2 (en) | 2018-10-29 | 2022-05-24 | Chromalloy Gas Turbine Llc | Method and apparatus for improving cooling of a turbine shroud |
WO2020092234A1 (en) * | 2018-10-29 | 2020-05-07 | Chromalloy Gas Turbine Llc | Method and apparatus for improving cooling of a turbine shroud |
US11352889B2 (en) * | 2018-12-18 | 2022-06-07 | General Electric Company | Airfoil tip rail and method of cooling |
US11225872B2 (en) | 2019-11-05 | 2022-01-18 | General Electric Company | Turbine blade with tip shroud cooling passage |
DE102019129835A1 (de) | 2019-11-06 | 2021-05-06 | Man Energy Solutions Se | Vorrichtung zur Kühlung eines Bauteils einer Gasturbine/Strömungsmaschine mittels Prallkühlung |
JP7477284B2 (ja) | 2019-11-14 | 2024-05-01 | 三菱重工業株式会社 | タービン翼及びガスタービン |
US11629642B2 (en) | 2019-12-20 | 2023-04-18 | General Electric Company | System and methods for igniting and operating a gas turbine engine with alternative fuels |
CN111852575A (zh) * | 2020-07-27 | 2020-10-30 | 北京全四维动力科技有限公司 | 涡轮转子叶片及包括其的燃气轮机 |
Family Cites Families (15)
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GB1514613A (en) | 1976-04-08 | 1978-06-14 | Rolls Royce | Blade or vane for a gas turbine engine |
GB2223276B (en) * | 1988-09-30 | 1992-09-02 | Rolls Royce Plc | Turbine aerofoil blade |
JPH02221602A (ja) * | 1989-02-23 | 1990-09-04 | Toshiba Corp | タービン動翼 |
JPH03194101A (ja) * | 1989-12-21 | 1991-08-23 | Toshiba Corp | ガスタービン冷却動翼 |
US5122033A (en) * | 1990-11-16 | 1992-06-16 | Paul Marius A | Turbine blade unit |
US5482435A (en) | 1994-10-26 | 1996-01-09 | Westinghouse Electric Corporation | Gas turbine blade having a cooled shroud |
JP3035187B2 (ja) * | 1995-05-09 | 2000-04-17 | 東北電力株式会社 | ガスタービン中空冷却動翼 |
EP1013884B1 (de) * | 1998-12-24 | 2005-07-27 | ALSTOM Technology Ltd | Turbinenschaufel mit aktiv gekühltem Deckbandelememt |
EP1041247B1 (en) * | 1999-04-01 | 2012-08-01 | General Electric Company | Gas turbine airfoil comprising an open cooling circuit |
US6761534B1 (en) | 1999-04-05 | 2004-07-13 | General Electric Company | Cooling circuit for a gas turbine bucket and tip shroud |
DE19963377A1 (de) * | 1999-12-28 | 2001-07-12 | Abb Alstom Power Ch Ag | Turbinenschaufel mit aktiv gekühltem Deckbandelement |
US6471480B1 (en) * | 2001-04-16 | 2002-10-29 | United Technologies Corporation | Thin walled cooled hollow tip shroud |
US6869270B2 (en) * | 2002-06-06 | 2005-03-22 | General Electric Company | Turbine blade cover cooling apparatus and method of fabrication |
US6811378B2 (en) * | 2002-07-31 | 2004-11-02 | Power Systems Mfg, Llc | Insulated cooling passageway for cooling a shroud of a turbine blade |
US7686581B2 (en) | 2006-06-07 | 2010-03-30 | General Electric Company | Serpentine cooling circuit and method for cooling tip shroud |
-
2007
- 2007-01-12 US US11/652,483 patent/US7568882B2/en active Active
-
2008
- 2008-01-07 CH CH00014/08A patent/CH703144B1/de not_active IP Right Cessation
- 2008-01-08 DE DE102008003412.6A patent/DE102008003412B4/de active Active
- 2008-01-11 JP JP2008003924A patent/JP5546732B2/ja active Active
- 2008-01-11 CN CN2008100029019A patent/CN101235728B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
US7568882B2 (en) | 2009-08-04 |
JP2008169845A (ja) | 2008-07-24 |
CH703144B1 (de) | 2011-11-30 |
DE102008003412B4 (de) | 2024-02-29 |
DE102008003412A1 (de) | 2008-07-17 |
CN101235728B (zh) | 2013-05-01 |
US20080170946A1 (en) | 2008-07-17 |
CN101235728A (zh) | 2008-08-06 |
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